Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Leonardo AW119 Lightweight Single-Engine Utility Helicopter.
1 x Pratt & Whitney Canada (PWC) PT6B-37A turboshaft engine developing 1,000 horsepower while driving a four-bladed main rotor and two-bladed tail rotor unit (facing port side).
Propulsion
177 mph
285 kph | 154 kts
Max Speed
15,010 ft
4,575 m | 3 miles
Service Ceiling
593 miles
955 km | 516 nm
Operational Range
1,800 ft/min
549 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).